Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7/
| Main Author: | |
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| Corporate Authors: | , , |
| Format: | Book |
| Language: | English |
| Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1985
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| Series: | NASA technical paper
2307 |
| Subjects: |
| Physical Description: | 47 σ. : έγχρ. εικ. ; 27 εκ. |
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